Aerothermodynamic and Scramjet Tests in High Enthalpy Shock Tunnel
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1041
Reference13 articles.
1. 2HornungHG,PerformancedataoftheNewFree-PistonShockTunnelatGALCIT, AIAA92-3943.1992.
2. AIAA 01-1824. 2001.
3. AIAA 01-1768. 2001
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